Výsledky vyhledávání - "液体推薬ロケットエンジン"

Integrated design methodology for highly reliable liquid rocket engine: Optimizing process of concept design quality. Failure simulation at start trangent

Autor: Aoki, Hiroshi, Taguchi, Hideyuki, Kuratani, Naoshi, Okai, Keiichi, Kojima, Takayuki, Hasegawa, Takuya, Kanda, Takeshi

Publikováno v: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems. :25-30

In past, the Design for Space Systems has conducted accumulating the optimum design results for each device. 'System Reliability Level' was measured as the results of long time development tests. Recently, the new design method is required. It is nec

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7b060bedcd042b237dcce7adbde54a66
http://id.nii.ac.jp/1696/00006230/

Zobrazit plný text záznamu

ロケットエンジン噴射器流れの数値解析

Autor: Shimizu, Kazuya, Shimizu, Taro

Numerical study on the jet flow in a high pressure fluid has been conducted in order to simulate atomization, mixing and combustion in a liquid rocket engine combustion chamber. The simulation results successfully show the break-up process of liquid

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3f1321bd8fb2f6a1eb68e663b9140d51
http://id.nii.ac.jp/1696/00006226/

Zobrazit plný text záznamu

Numerical analysis of propellant feed systems in liquid-propellant rocket engines

Autor: Negishi, Hideyo, Tani, Naoki, Yamanishi, Nobuhiro

Numerical simulator for propellant feed systems in liquid-propellant rocket engines based on CFD is under development for supporting H-2A rocket and next generation rocket development. This simulator consists of turbo pump system simulator and tank s

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::90cebffcaf5813c84504cb22f9f0b2c5
http://id.nii.ac.jp/1696/00006227/

Zobrazit plný text záznamu

Numerical simulation of LE-7A engine turbine flow

Autor: Saiki, Kazuhisa, Nozaki, Osamu

Publikováno v: 宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004. :160-165

The fuel turbo pump (FTP) of LE-7A engine had vibration problem of turbine rotor system. The turbine consists of 33 nozzle vanes, 58 rotor blades, 36 stator vanes and an upstream manifold. The manifold has 30 radial slits between a volute and a downs

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::91f4ec9ba4271cf9d0b72deaf6faf1ac
http://id.nii.ac.jp/1696/00006461/

Zobrazit plný text záznamu

Rocket engine dynamic simulator (REDS)

Autor: Kimura, Toshiya, Takahashi, Masahiro, Wakamatsu, Yoshio, Hasegawa, Keiichi, Yamanishi, Nobuhiro

Publikováno v: 宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003. :107-112

The Rocket Engine Dynamic Simulator (REDS) has been developed. REDS is a kind of simulation tool to simulate and examine unsteady behavior of a rocket engine. A rocket engine is modeled as a system of pipes with various hydraulic elements such as tur

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::dba89e51a73c3d0458ab5266388bcbc7
http://id.nii.ac.jp/1696/00006615/

Zobrazit plný text záznamu

Research on the health monitoring of a liquid rocket propulsion system

Autor: Makino, Takashi, Akiyama, Masao, Tamura, Naoki, Oya, Koji, Kawabe, Shunji

Publikováno v: 宇宙輸送シンポジウム平成14年度 = Proceedings of Space Transportation Symposium FY2002. :125-128

資料番号: AA0045426031

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::69a20a7cb146455bf875401fd8b045a6
http://id.nii.ac.jp/1696/00017361/

Zobrazit plný text záznamu

Three dimensional numerical analysis on the lateral force generated at a rocket nozzle

Autor: Shimizu, Taro, Miyajima, Hiroshi, Kodera, Masatoshi

Publikováno v: 宇宙輸送シンポジウム平成14年度 = Proceedings of Space Transportation Symposium FY2002. :95-98

資料番号: AA0045426024

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2d39993ed0e16c0301ef0e0efe745494
http://id.nii.ac.jp/1696/00017354/

Zobrazit plný text záznamu

Research on reusable rockets and scientific observation

Autor: Inatani, Yoshifumi

Publikováno v: 第3回宇宙科学シンポジウム = Proceedings of the 3rd Space Science Symposium. :377-380

資料番号: AA0045981040

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::0b84c24e814674653509bd0c56d00f34
http://id.nii.ac.jp/1696/00011685/

Zobrazit plný text záznamu

Results of the development of a 500 N-class 2-liquid apogee engine

Autor: Kajiwara, Kenichi, Saito, Kenkichi, Masuda, Ideo, Iihara, Shigeyasu, Umeda, Joji

Publikováno v: 宇宙輸送シンポジウム平成14年度 = Proceedings of Space Transportation Symposium FY2002. :17-20

資料番号: AA0045426005

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ca4a589b4b6bfe989a795d259d40136b
http://id.nii.ac.jp/1696/00017335/

Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání